An aircraft (100) includes a body (10) and an outer frame (1) rotatably coupled to the body (10). The body (10) includes a plurality of rotary blades (15a-15d) and a driver (14a-14d) configured to rotate the plurality of rotary blades (15a-15d). The outer frame (1) includes a rotary frame (1a-1c) rotatable about a rotation axis intersecting the direction of gravity, and a center of gravity of the plurality of rotary blades (15a-15d) and the driver (14a-14d) is located lower than the rotation axis in the direction of gravity.


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    Titel :

    AIRCRAFT, FLIGHT SYSTEM, AND STRUCTURE INSPECTION SYSTEM


    Weitere Titelangaben:

    FLUGZEUG, FLUGSYSTEM UND STRUKTURINSPEKTIONSSYSTEM
    AÉRONEF, SYSTÈME DE VOL ET SYSTÈME D'INSPECTION DE STRUCTURE


    Beteiligte:
    KAWAKAMI AKIHIRO (Autor:in) / TEZUKA SHINJI (Autor:in)

    Erscheinungsdatum :

    24.01.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64U



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